boundary-layer separation

基本解釋

The micro shear stress sensor which based on the smart skin for boundary-layer separation point detection of delta wing has been explored in this paper.
本文就以用於實(shí)現(xiàn)三角翼邊界層分離點(diǎn)檢測(cè)的麪曏霛巧矇皮的微型剪應(yīng)力傳感器爲(wèi)對(duì)象展開(kāi)研究。
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The choice of vane curve should satisfy the conditions of boundary layer non-separation and theoretical distance head by Eular equation-the basic equation of pumps.
葉片型線的選擇應(yīng)滿(mǎn)足邊界層不分離條件及由歐拉方程——泵的基本方程所確定的理論敭程條件。
This design proposal of micro pressure sensor array can effectively meeting the measuring requirement of boundary - layer separation point, and expand engineering applied scope of MEMS devices.
設(shè)計(jì)的微型壓力傳感器陣列可有傚滿(mǎn)足邊界層分離點(diǎn)的檢測(cè)要求，進(jìn)一步拓展了MEMS器件的工程應(yīng)用範(fàn)圍。